(2)
A task to install the float valve for the fuel vent system.
TASK 28-13-11-004-001
2. Fuel Vent Float Valve Removal (Fig. 401)
_____________________________
A. References
(1)
AMM 28-10-00/201, Fuel Storage
(2)
AMM 28-11-11/401, Wing Fuel Tank Access Panels
(3)
AMM 28-11-31/401, Center Tank Access Panels
B. Access
(1)
Location Zones
221 Center Section Fuel Tank
305 Left Wing Fuel Tank
405 Right Wing Fuel Tank
(2)
Access Panels
7214 Fuel Tank Access Door
7414 Fuel Tank Access Door
C. Procedure
S 654-002
WARNING: CAREFULLY DO ALL THE SAFETY PROCEDURES TO DEFUEL THE TANK AND
_______ TO GO INTO IT. INJURY TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR IF YOU DO NOT FOLLOW THE SAFETY PROCEDURES.
(1)
Prepare the applicable fuel tank for entry (AMM 28-10-00/201).
S 014-003
(2)
Remove the access panels for the applicable tank to get access to the float valve (AMM 28-11-11/401, AMM 28-11-31/401).
(3)
Remove the bolts that attach the float valve to the structure.
(4)
Remove the float valve.
S 034-004
S 024-005
TASK 28-13-11-404-006
3. Fuel Vent Float Valve Installation (Fig. 401)
__________________________________
A. References
(1) AMM 28-11-11/401, Wing Fuel Tank Access Panels
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-13-11
ALL ú ú 02 Page 401 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
(RIGHT WING SHOWN LEFT WING OPPOSITE)
Fuel Vent Float Valve Installation
Figure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-13-11
ALL ú ú 01 Page 402 ú Jun 25/84
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
(2) AMM 28-11-31/401, Center Tank Access Panels
B. Access
(1)
Location Zones
221 Center Section Fuel Tank
305 Left Wing Fuel Tank
405 Right Wing Fuel Tank
(2)
Access Panels
7214 Fuel Tank Access Door
7414 Fuel Tank Access Door
C. Procedure
S 434-007
(1)
Install the O-ring in the O-ring groove on the float valve.
S 424-008
(2)
Hold the float valve in the correct position and install the bolts.
S 214-009
(3)
Make sure there is no color identification tape on the components in the fuel tank.
(4)
Make sure the tank is clean.
S 414-011
(5)
Install the access panels that you removed before this step
(AMM 28-11-11/401, AMM 28-11-31/401).
S 214-010
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-13-11
ALL ú ú 01 Page 403 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
SHROUD DRAIN LINE - INSPECTION/CHECK
____________________________________
1. General_______
A. This procedure has one task. The task is to drain the APU shroud space. Drain the shroud space regularly to find collected fluids which did not go out of the drain mast. You can also examine the fluids for too much fuel. Too much fuel in the collected fluid shows a leak in the APU fuel line or the auxiliary fuel tank. The auxiliary fuel cavity drain line is interconnected to the APU shroud drain mast.
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 燃油 FUEL 2(5)
